Vacuum adiabatic body and refrigerator

ABSTRACT

Provided is a vacuum adiabatic body. To reduce a heat transfer amount between two plates, the vacuum adiabatic body includes: a conductive resistance sheet connecting plate members to each other, an exhaust port through which a gas of a third space is exhausted, and a sealing frame covering a conductive resistance sheet. A virtual line connecting both end portions of the conductive resistance sheet to each other is installed to be obliquely inclined when at least one extension direction of a first plate member or a second plate member is viewed in a horizontal direction.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a Continuation Application of prior U.S. Pat.Application Serial No. 16/980,599 filed Sep. 14, 2020, which is a U.S.National Stage Application under 35 U.S.C. §371 of PCT Application No.PCT/KR2019/007757, filed Jun. 26, 2019, which claims priority to KoreanPatent Application No. 10-2018-0074232, filed Jun. 27, 2018, whoseentire disclosures are hereby incorporated by reference.

BACKGROUND 1. Field

The present disclosure relates to a vacuum adiabatic body and arefrigerator.

2. Background

A vacuum adiabatic body is a product for suppressing heat transfer byvacuumizing the interior of a body thereof. The vacuum adiabatic bodymay reduce heat transfer by convection and conduction, and hence isapplied to heating apparatuses and refrigerating apparatuses. In atypical adiabatic method applied to a refrigerator, although it isdifferently applied in refrigeration and freezing, a foam urethaneadiabatic wall having a thickness of about 30 mm or more is generallyprovided. However, the internal volume of the refrigerator is thereforereduced.

In order to increase the internal volume of a refrigerator, there is anattempt to apply a vacuum adiabatic body to the refrigerator.

First, Korean Patent No. 10-0343719 (Cited Document 1) of the presentapplicant has been disclosed. According to Reference Document 1, thereis disclosed a method in which a vacuum adiabatic panel is prepared andthen built in walls of a refrigerator, and the exterior of the vacuumadiabatic panel is finished with a separate molding as Styrofoam.According to the method, additional foaming is not required, and theadiabatic performance of the refrigerator is improved. However,fabrication cost is increased, and a fabrication method is complicated.

As another example, a technique of providing walls using a vacuumadiabatic material and additionally providing adiabatic walls using afoam filling material has been disclosed in Korean Patent PublicationNo. 10-2015-0012712 (Cited Document 2). According to Reference Document2, fabrication cost is increased, and a fabrication method iscomplicated.

As further another example, there is an attempt to fabricate all wallsof a refrigerator using a vacuum adiabatic body that is a singleproduct. For example, a technique of providing an adiabatic structure ofa refrigerator to be in a vacuum state has been disclosed in U.S. Pat.Laid-Open Publication No. US20040226956A1 (Reference Document 3).However, it is difficult to obtain a practical level of an adiabaticeffect by providing a wall of the refrigerator with sufficient vacuum.In detail, there are limitations that it is difficult to prevent a heattransfer phenomenon at a contact portion between an outer case and aninner case having different temperatures, it is difficult to maintain astable vacuum state, and it is difficult to prevent deformation of acase due to a negative pressure of the vacuum state. Due to theselimitations, the technology disclosed in Reference Document 3 is limitedto a cryogenic refrigerator, and does not provide a level of technologyapplicable to general households.

Alternatively, the present applicant has applied for Korean PatentPublication No. 10-2017-0016187 (Cited Document 4) that discloses avacuum adiabatic body and a refrigerator. According to the presentdisclosure, both the door and the main body of the refrigerator areprovided as a vacuum adiabatic body, and a large adiabatic material isadded to the edge of the door to prevent cold air from leaking from theedge of the main body and the door. However, there is a limitation inthat manufacturing is complicated, and an internal volume of therefrigerator is greatly reduced. Also, since the internal space of thevacuum adiabatic body is empty in a vacuum state, there is a limitationthat deformation such as bending or buckling occurs due to weak strengthwhen compared to an article filled with a resin material such aspolyurethane according to the related art.

To solve the above-mentioned limitations, the applicant of the presentdisclosure has applied for Korean Patent Application No. 10-2017-0171616(Cited Document 5). According to this technology, a separate sealingframe is added to increase the internal space of the vacuum adiabaticbody and enhance the adiabatic performance between the body and thedoor.

According to Cited Document 5, the internal volume of the refrigeratorincreases, but a contact area between a gasket and the sealing frame isstill narrow, and thus, sufficient adiabatic performance may not beachieved. Also, there is a limitation in that it is difficult to form anenergy nose as an adiabatic gap part due to an air layer, not onlysealing by contact of the gasket, resulting in deterioration ofadiabatic efficiency.

The above references are incorporated by reference herein whereappropriate for appropriate teachings of additional or alternativedetails, features and/or technical background.

Disclosure Technical Problem

Embodiments provide a refrigerator to which a vacuum adiabatic bodyhaving a narrow adiabatic interval is applied and in which an adiabaticinterval due to contact between a door and a main body more increases.

Embodiments also provide a refrigerator to which a vacuum adiabatic bodyhaving a narrow adiabatic interval is applied and in which an energynose realized in an air layer having a narrow width in a contactinterval between a door and a main body is sufficiently secured.

Embodiment s also provide in which a refrigerator to which a vacuumadiabatic body is applied and in which heat loss due to thermalconduction passing through a conductive resistance sheet is reduced.

Technical Solution

In one embodiment, a vacuum adiabatic body includes: a conductiveresistance sheet provided on a contact surface of a pair of platemembers constituting a wall of the vacuum adiabatic body to blockthermal conduction between the plate members; and a sealing frameconfigured to cover the conductive resistance sheet, wherein a virtualline connecting both end portions of the conductive resistance sheet toeach other is installed to be obliquely inclined when at least oneextension direction of a first plate member or a second plate member isviewed in a horizontal direction. According to an embodiment, conductiveheat transfer may be more reduced to improve adiabatic efficiency of arefrigerator.

In another embodiment, a refrigerator includes: a gasket installed onthe door or the main body to seal a potion at which the door and themain body contact each other; and a sealing frame contacting the gasketas a member corresponding to the gasket, the sealing frame beingdisposed between the third space and the door, wherein the gasketincludes: a gasket body contacting the sealing frame to seal a gapbetween the door and the main body; and a gasket coupling tool disposedto be obliquely inclined with respect to an extension direction of thegasket body. According to an embodiment, an adiabatic interval maysignificantly increase to improve adiabatic efficiency.

A heat resistance unit that resists heat transfer between plate membersmay include a conductive resistance sheet that resists conduction ofheat transferred along a wall of the vacuum space part and may furtherinclude a side frame coupled to the conductive resistance sheet.

Also, the heat resistance unit may include at least one radiationresistance sheet that is provided in a plate shape within the vacuumspace part or may include a porous material that resists radiation heattransfer between the second plate member and the first plate memberwithin the vacuum space part.

Advantageous Effects

According to the embodiments, since the contact part between the doorand the main body is provided to be inclined, the adiabatic interval dueto the contact may more increase, and the thermal conduction passingthrough the contact portion may be greatly reduced.

According to the embodiments, after the contact part between the doorand the main body, the energy nose may be secured to be sufficientlylong, and the adiabatic effect may more increase.

According to the embodiments, the length of the conductive resistancesheet provided at the same interval becomes longer so that theconductive heat loss of the vacuum adiabatic body may be reduced, andthe energy consumption efficiency of the refrigerator may be furtherimproved.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a perspective view of a refrigerator according to anembodiment.

FIG. 2 is a view schematically showing a vacuum adiabatic body used in amain body and a door of the refrigerator.

FIG. 3 is a view illustrating various embodiments of an internalconfiguration of a vacuum space part.

FIG. 4 is a view illustrating various embodiments of conductiveresistance sheets and peripheral portions thereof.

FIG. 5 is a graph illustrating a variation in adiabatic performance anda variation in gas conductivity according to a vacuum pressure byapplying a simulation.

FIG. 6 is a graph illustrating results obtained by observing a time anda pressure in a process of exhausting the inside of the vacuum adiabaticbody when a supporting unit is used.

FIG. 7 is a graph illustrating results obtained by comparing a vacuumpressure with gas conductivity.

FIG. 8 is a cross-sectional perspective view of an edge of the vacuumadiabatic body.

FIGS. 9 and 10 are schematic front views of a main body in a virtualstate in which an inner surface part is spread.

FIG. 11 is a cross-sectional view of a contact part in a state in whichthe main body is closed by the door.

FIG. 12 is a cross-sectional view illustrating a contact part of a mainbody and a door according to another embodiment.

FIGS. 13 and 14 are partial cutaway perspective views of an innersurface part, wherein FIG. 13 illustrates in a state in which couplingis completed, and FIG. 14 illustrates a coupling process.

FIG. 15 is a view for sequentially explaining coupling of a sealingframe when the sealing frame is provided as two members according to anembodiment.

FIGS. 16 and 17 are views illustrating one end portion of the sealingframe, wherein FIG. 16 illustrates a state before a door hinge isinstalled, and FIG. 17 illustrates a state in which the door hinge isinstalled.

FIG. 18 is a view for explaining an effect of the sealing frameaccording to an embodiment in comparison with the technique according tothe related art, wherein FIG. 18(a) is a cross-sectional view of acontact part of a main body-side vacuum adiabatic body and a dooraccording to an embodiment, and FIG. 18(b) is a cross-sectional view ofa main body and a door according to the related art.

FIGS. 19 to 24 are views illustrating various embodiments in which thesealing frame is installed.

FIG. 25 is an enlarged cross-sectional view illustrating a contact partbetween a door and a main body of the refrigerator as an edge portion ofa vacuum adiabatic body according to an embodiment.

FIG. 26 is a conceptual view of an energy nose in the refrigerator.

FIG. 27 is a view for comparing the energy noses of a general conductiveresistance sheet and an inclined conductive resistance sheet.

FIG. 28 is a view for explaining a welding device that welds aconductive resistance sheet to a plate member according to a relatedart.

FIG. 29 is a view for comparing coupling processes of the conductiveresistance sheet according to the foregoing embodiment and theconductive resistance sheet according to this embodiment.

FIG. 30 is a comparison view of a gasket.

FIG. 31 is an enlarged cross-sectional view illustrating a contact partbetween a door and a main body of the refrigerator as an edge portion ofa vacuum adiabatic body according to another embodiment.

DETAILED DESCRIPTION

Hereinafter, exemplary embodiments will be described with reference tothe accompanying drawings. The invention may, however, be embodied inmany different forms and should not be construed as being limited to theembodiments set forth herein, and a person of ordinary skill in the art,who understands the spirit of the present invention, may readilyimplement other embodiments included within the scope of the sameconcept by adding, changing, deleting, and adding components; rather, itwill be understood that they are also included within the scope of thepresent invention.

The drawings shown below may be displayed differently from the actualproduct, or exaggerated or simple or detailed parts may be deleted, butthis is intended to facilitate understanding of the technical idea ofthe present invention. It should not be construed as limited. However,it will try to show the actual shape as much as possible.

The following embodiments may be applied to the description of anotherembodiment unless the other embodiment does not collide with each other,and some configurations of any one of the embodiments may be modified ina state in which only a specific portion is modified in anotherconfiguration may be applied.

In the following description, the vacuum pressure means any pressurestate lower than the atmospheric pressure. In addition, the expressionthat a vacuum degree of A is higher than that of B means that a vacuumpressure of A is lower than that of B.

FIG. 1 is a perspective view of a refrigerator according to anembodiment.

Referring to FIG. 1 , the refrigerator 1 includes a main body 2 providedwith a cavity 9 capable of storing storage goods and a door 3 providedto open/close the main body 2. The door 3 may be rotatably or slidablymovably disposed to open/close the cavity 9. The cavity 9 may provide atleast one of a refrigerating compartment and a freezing compartment.

Parts constituting a freezing cycle in which cold air is supplied intothe cavity 9. In detail, the parts include a compressor 4 forcompressing a refrigerant, a condenser 5 for condensing the compressedrefrigerant, an expander 6 for expanding the condensed refrigerant, andan evaporator 7 for evaporating the expanded refrigerant to take heat.As a typical structure, a fan may be installed at a position adjacent tothe evaporator 7, and a fluid blown from the fan may pass through theevaporator 7 and then be blown into the cavity 9. A freezing load iscontrolled by adjusting the blowing amount and blowing direction by thefan, adjusting the amount of a circulated refrigerant, or adjusting thecompression rate of the compressor, so that it is possible to control arefrigerating space or a freezing space.

FIG. 2 is a view schematically showing a vacuum adiabatic body used inthe main body and the door of the refrigerator. In FIG. 2 , a mainbody-side vacuum adiabatic body is illustrated in a state in which topand side walls are removed, and a door-side vacuum adiabatic body isillustrated in a state in which a portion of a front wall is removed. Inaddition, sections of portions at conductive resistance sheets areprovided are schematically illustrated for convenience of understanding.

Referring to FIG. 2 , the vacuum adiabatic body includes a first platemember 10 for providing a wall of a low-temperature space, a secondplate member 20 for providing a wall of a high-temperature space, avacuum space part 50 defined as an interval part between the first andsecond plate members 10 and 20. Also, the vacuum adiabatic body includesthe conductive resistance sheets 60 and 63 for preventing thermalconduction between the first and second plate members 10 and 20. Asealing part 61 for sealing the first and second plate members 10 and 20is provided such that the vacuum space part 50 is in a sealing state.When the vacuum adiabatic body is applied to a refrigerating or heatingcabinet, the first plate member 10 may be referred to as an inner case,and the second plate member 20 may be referred to as an outer case. Amachine room 8 in which parts providing a freezing cycle areaccommodated is placed at a lower rear side of the main body-side vacuumadiabatic body, and an exhaust port 40 for forming a vacuum state byexhausting air in the vacuum space part 50 is provided at any one sideof the vacuum adiabatic body. In addition, a pipeline 64 passing throughthe vacuum space part 50 may be further installed so as to install adefrosting water line and electric lines.

The first plate member 10 may define at least one portion of a wall fora first space provided thereto. The second plate member 20 may define atleast one portion of a wall for a second space provided thereto. Thefirst space and the second space may be defined as spaces havingdifferent temperatures. Here, the wall for each space may serve as notonly a wall directly contacting the space but also a wall not contactingthe space. For example, the vacuum adiabatic body of the embodiment mayalso be applied to a product further having a separate wall contactingeach space.

Factors of heat transfer, which cause loss of the adiabatic effect ofthe vacuum adiabatic body, are thermal conduction between the first andsecond plate members 10 and 20, heat radiation between the first andsecond plate members 10 and 20, and gas conduction of the vacuum spacepart 50.

Hereinafter, a heat resistance unit provided to reduce adiabatic lossrelated to the factors of the heat transfer will be provided. Meanwhile,the vacuum adiabatic body and the refrigerator of the embodiment do notexclude that another adiabatic means is further provided to at least oneside of the vacuum adiabatic body. Therefore, an adiabatic means usingfoaming or the like may be further provided to another side of thevacuum adiabatic body.

The heat resistance unit may include a conductive resistance sheet thatresists conduction of heat transferred along a wall of a third space andmay further include a side frame coupled to the conductive resistancesheet. The conductive resistance sheet and the side frame will beclarified by the following description.

Also, the heat resistance unit may include at least one radiationresistance sheet that is provided in a plate shape within the thirdspace or may include a porous material that resists radiation heattransfer between the second plate member and the first plate memberwithin the third space. The radiation resistance sheet and the porousmaterial will be clarified by the following description.

FIG. 3 is a view illustrating various embodiments of an internalconfiguration of the vacuum space part.

First referring to FIG. 3A, the vacuum space part 50 may be provided ina third space having a pressure different from that of each of the firstand second spaces, preferably, a vacuum state, thereby reducing anadiabatic loss. The third space may be provided at a temperature betweenthe temperature of the first space and the temperature of the secondspace. Since the third space is provided as a space in the vacuum state,the first and second plate members 10 and 20 receive a force contractingin a direction in which they approach each other due to a forcecorresponding to a pressure difference between the first and secondspaces. Therefore, the vacuum space part 50 may be deformed in adirection in which it is reduced. In this case, the adiabatic loss maybe caused due to an increase in amount of heat radiation, caused by thecontraction of the vacuum space part 50, and an increase in amount ofthermal conduction, caused by contact between the plate members 10 and20.

The supporting unit 30 may be provided to reduce deformation of thevacuum space part 50. The supporting unit 30 includes a bar 31. The bar31 may extend in a substantially vertical direction with respect to theplate members to support a distance between the first plate member andthe second plate member. A support plate 35 may be additionally providedon at least any one end of the bar 31. The support plate 35 may connectat least two or more bars 31 to each other to extend in a horizontaldirection with respect to the first and second plate members 10 and 20.The support plate 35 may be provided in a plate shape or may be providedin a lattice shape so that an area of the support plate contacting thefirst or second plate member 10 or 20 decreases, thereby reducing heattransfer. The bars 31 and the support plate 35 are fixed to each otherat at least one portion, to be inserted together between the first andsecond plate members 10 and 20. The support plate 35 contacts at leastone of the first and second plate members 10 and 20, thereby preventingdeformation of the first and second plate members 10 and 20. Inaddition, based on the extension direction of the bars 31, a totalsectional area of the support plate 35 is provided to be greater thanthat of the bars 31, so that heat transferred through the bars 31 may bediffused through the support plate 35.

The supporting unit 30 may be made of a resin selected from PC, glassfiber PC, low outgassing PC, PPS, and LCP to obtain high compressivestrength, a low outgassing and water absorption rate, low thermalconductivity, high compressive strength at a high temperature, andsuperior processability.

A radiation resistance sheet 32 for reducing heat radiation between thefirst and second plate members 10 and 20 through the vacuum space part50 will be described. The first and second plate members 10 and 20 maybe made of a stainless material capable of preventing corrosion andproviding a sufficient strength. The stainless material has a relativelyhigh emissivity of 0.16, and hence a large amount of radiation heat maybe transferred. In addition, the supporting unit 30 made of the resinhas a lower emissivity than the plate members, and is not entirelyprovided to inner surfaces of the first and second plate members 10 and20. Hence, the supporting unit 30 does not have great influence onradiation heat. Therefore, the radiation resistance sheet 32 may beprovided in a plate shape over a majority of the area of the vacuumspace part 50 so as to concentrate on reduction of radiation heattransferred between the first and second plate members 10 and 20. Aproduct having a low emissivity may be preferably used as the materialof the radiation resistance sheet 32. In an embodiment, an aluminum foilhaving an emissivity of 0.02 may be used as the radiation resistancesheet 32. Also, since the transfer of radiation heat may not besufficiently blocked using one radiation resistance sheet, at least tworadiation resistance sheets 32 may be provided at a certain distance soas not to contact each other. Also, at least one radiation resistancesheet may be provided in a state in which it contacts the inner surfaceof the first or second plate member 10 or 20.

Referring to FIG. 3B, the distance between the plate members ismaintained by the supporting unit 30, and a porous material 33 may befilled in the vacuum space part 50. The porous material 33 may have ahigher emissivity than the stainless material of the first and secondplate members 10 and 20. However, since the porous material 33 is filledin the vacuum space part 50, the porous material 33 has a highefficiency for resisting the radiation heat transfer.

In the present embodiment, the vacuum adiabatic body may be manufacturedwithout the radiation resistance sheet 32.

Referring to FIG. 3C, the supporting unit 30 for maintaining the vacuumspace part 50 may not be provided. A porous material 333 may be providedto be surrounded by a film 34 instead of the supporting unit 30. Here,the porous material 33 may be provided in a state of being compressed sothat the interval of the vacuum space part is maintained. The film 34made of, for example, a PE material may be provided in a state in whicha hole is punched in the film 34.

In the present embodiment, the vacuum adiabatic body may be manufacturedwithout the supporting unit 30. That is to say, the porous material 33may perform the function of the radiation resistance sheet 32 and thefunction of the supporting unit 30 together.

FIG. 4 is a view illustrating various embodiments of conductiveresistance sheets and peripheral parts thereof. Structures of theconductive resistance sheets are briefly illustrated in FIG. 2 , butwill be understood in detail with reference to the drawings.

First, a conductive resistance sheet proposed in FIG. 8A may bepreferably applied to the main body-side vacuum adiabatic body.Specifically, the first and second plate members 10 and 20 are to besealed so as to vacuumize the interior of the vacuum adiabatic body. Inthis case, since the two plate members have different temperatures fromeach other, heat transfer may occur between the two plate members. Aconductive resistance sheet 60 is provided to prevent thermal conductionbetween two different kinds of plate members.

The conductive resistance sheet 60 may be provided with the sealing part61 at which both ends of the conductive resistance sheet 60 are sealedto defining at least one portion of the wall for the third space andmaintain the vacuum state. The conductive resistance sheet 60 may beprovided as a thin foil in unit of micrometer so as to reduce the amountof heat conducted along the wall for the third space. The sealing parts610 may be provided as welding parts. That is, the conductive resistancesheet 60 and the plate members 10 and 20 may be fused to each other. Inorder to cause a fusing action between the conductive resistance sheet60 and the plate members 10 and 20, the conductive resistance sheet 60and the plate members 10 and 20 may be made of the same material, and astainless material may be used as the material. The sealing parts 610are not limited to the welding parts, and may be provided through aprocess such as cocking. The conductive resistance sheet 60 may beprovided in a curved shape. Thus, a thermal conduction distance of theconductive resistance sheet 60 is provided longer than the lineardistance of each plate member, so that the amount of thermal conductionmay be further reduced.

A change in temperature occurs along the conductive resistance sheet 60.Therefore, in order to block heat transfer to the exterior of theconductive resistance sheet 60, a shielding part 62 may be provided atthe exterior of the conductive resistance sheet 60 such that anadiabatic action occurs. In other words, in the refrigerator, the secondplate member 20 has a high temperature and the first plate member 10 hasa low temperature. In addition, thermal conduction from high temperatureto low temperature occurs in the conductive resistance sheet 60, andhence the temperature of the conductive resistance sheet 60 is suddenlychanged. Therefore, when the conductive resistance sheet 60 is opened tothe exterior thereof, heat transfer through the opened place mayseriously occur. In order to reduce heat loss, the shielding part 62 isprovided at the exterior of the conductive resistance sheet 60. Forexample, when the conductive resistance sheet 60 is exposed to any oneof the low-temperature space and the high-temperature space, theconductive resistance sheet 60 does not serve as a conductive resistoras well as the exposed portion thereof, which is not preferable.

The shielding part 62 may be provided as a porous material contacting anouter surface of the conductive resistance sheet 60. The shielding part62 may be provided as an adiabatic structure, e.g., a separate gasket,which is placed at the exterior of the conductive resistance sheet 60.The shielding part 62 may be provided as a portion of the vacuumadiabatic body, which is provided at a position facing a correspondingconductive resistance sheet 60 when the main body-side vacuum adiabaticbody is closed with respect to the door-side vacuum adiabatic body. Inorder to reduce heat loss even when the main body and the door areopened, the shielding part 62 may be preferably provided as a porousmaterial or a separate adiabatic structure.

A conductive resistance sheet proposed in FIG. 4(b) may be preferablyapplied to the door-side vacuum adiabatic body. In FIG. 4(b), portionsdifferent from those of FIG. 4(a) are described in detail, and the samedescription is applied to portions identical to those of FIG. 4(a). Aside frame 70 is further provided at an outside of the conductiveresistance sheet 60. A part for sealing between the door and the mainbody, an exhaust port necessary for an exhaust process, a getter portfor vacuum maintenance, and the like may be placed on the side frame 70.This is because the mounting of parts is convenient in the mainbody-side vacuum adiabatic body, but the mounting positions of parts arelimited in the door-side vacuum adiabatic body.

In the door-side vacuum adiabatic body, it is difficult to place theconductive resistance sheet 60 at a front end portion of the vacuumspace part, i.e., a corner side portion of the vacuum space part. Thisis because, unlike the main body, a corner edge portion of the door isexposed to the exterior. In more detail, if the conductive resistancesheet 60 is placed at the front end portion of the vacuum space part,the corner edge portion of the door is exposed to the exterior, andhence there is a disadvantage in that a separate adiabatic part shouldbe configured so as to thermally insulate the conductive resistancesheet 60.

A conductive resistance sheet proposed in FIG. 4(c) may be preferablyinstalled in the pipeline passing through the vacuum space part. In FIG.4(c), portions different from those of FIGS. 4(a) and 4(b) are describedin detail, and the same description is applied to portions identical tothose of FIGS. 4(a) and 4(b). A conductive resistance sheet having thesame shape as that of FIG. 4(a), preferably, a wrinkled conductiveresistance sheet 63 may be provided at a peripheral portion of thepipeline 64. Accordingly, a heat transfer path may be lengthened, anddeformation caused by a pressure difference may be prevented. Inaddition, a separate shielding part may be provided to improve theadiabatic performance of the conductive resistance sheet.

A heat transfer path between the first and second plate members 10 and20 will be described with reference back to FIG. 4(a). Heat passingthrough the vacuum adiabatic body may be divided into surface conductionheat ① conducted along a surface of the vacuum adiabatic body, morespecifically, the conductive resistance sheet 60, supporter conductionheat ② conducted along the supporting unit 30 provided inside the vacuumadiabatic body, gas conduction heat ③ conducted through an internal gasin the vacuum space part, and radiation transfer heat ④ transferredthrough the vacuum space part.

The transfer heat may be changed depending on various depending onvarious design dimensions. For example, the supporting unit may bechanged such that the first and second plate members 10 and 20 mayendure a vacuum pressure without being deformed, the vacuum pressure maybe changed, the distance between the plate members may be changed, andthe length of the conductive resistance sheet may be changed. Thetransfer heat may be changed depending on a difference in temperaturebetween the spaces (the first and second spaces) respectively providedby the plate members. In the embodiment, a preferred configuration ofthe vacuum adiabatic body has been found by considering that its totalheat transfer amount is smaller than that of a typical adiabaticstructure formed by foaming polyurethane. In a typical refrigeratorincluding the adiabatic structure formed by foaming the polyurethane, aneffective heat transfer coefficient may be proposed as 19.6 mW/mK.

By performing a relative analysis on heat transfer amounts of the vacuumadiabatic body of the embodiment, a heat transfer amount by the gasconduction heat ③ may become smallest. For example, the heat transferamount by the gas conduction heat ③ may be controlled to be equal to orsmaller than 4% of the total heat transfer amount. A heat transferamount by solid conduction heat defined as a sum of the surfaceconduction heat ① and the supporter conduction heat ② is largest. Forexample, the heat transfer amount by the solid conduction heat may reach75% of the total heat transfer amount. A heat transfer amount by theradiation transfer heat ③ is smaller than the heat transfer amount bythe solid conduction heat but larger than the heat transfer amount ofthe gas conduction heat. For example, the heat transfer amount by theradiation transfer heat ③ may occupy about 20% of the total heattransfer amount.

According to such a heat transfer distribution, effective heat transfercoefficients (eK: effective K) (W/mK) of the surface conduction heat ①,the supporter conduction heat ②, the gas conduction heat ③, and theradiation transfer heat ④ may have an order of Math Equation 1.

$\begin{matrix}{\text{eK}_{\text{solid conduction heat}} > \text{eK}_{\text{radiation transfer heat}} > \text{eK}_{\text{gas conduction heat}}} & \text{­­­[Equation 1]}\end{matrix}$

Here, the effective heat transfer coefficient (eK) is a value that maybe measured using a shape and temperature differences of a targetproduct. The effective heat transfer coefficient (eK) is a value thatmay be obtained by measuring a total heat transfer amount and atemperature at least one portion at which heat is transferred. Forexample, a calorific value (W) is measured using a heating source thatmay be quantitatively measured in the refrigerator, a temperaturedistribution (K) of the door is measured using heats respectivelytransferred through a main body and an edge of the door of therefrigerator, and a path through which heat is transferred is calculatedas a conversion value (m), thereby evaluating an effective heat transfercoefficient.

The effective heat transfer coefficient (eK) of the entire vacuumadiabatic body is a value given by k=QL/AΔT. Here, Q denotes a calorificvalue (W) and may be obtained using a calorific value of a heater. Adenotes a sectional area (m2) of the vacuum adiabatic body, L denotes athickness (m) of the vacuum adiabatic body, and △T denotes a temperaturedifference.

For the surface conduction heat, a conductive calorific value may beobtained through a temperature difference (△T) between an entrance andan exit of the conductive resistance sheet 60 or 63, a sectional area(A) of the conductive resistance sheet, a length (L) of the conductiveresistance sheet, and a thermal conductivity (k) of the conductiveresistance sheet (the thermal conductivity of the conductive resistancesheet is a material property of a material and may be obtained inadvance). For the supporter conduction heat, a conductive calorificvalue may be obtained through a temperature difference (△T) between anentrance and an exit of the supporting unit 30, a sectional area (A) ofthe supporting unit, a length (L) of the supporting unit, and a thermalconductivity (k) of the supporting unit. Here, the thermal conductivityof the supporting unit is a material property of a material and may beobtained in advance. The sum of the gas conduction heat ③, and theradiation transfer heat ④ may be obtained by subtracting the surfaceconduction heat and the supporter conduction heat from the heat transferamount of the entire vacuum adiabatic body. A ratio of the gasconduction heat ③, and the radiation transfer heat ④ may be obtained byevaluating radiation transfer heat when no gas conduction heat exists byremarkably lowering a vacuum degree of the vacuum space part 50.

When a porous material is provided inside the vacuum space part 50,porous material conduction heat ⑤ may be a sum of the supporterconduction heat ② and the radiation transfer heat ④. The porous materialconduction heat may be changed depending on various variables includinga kind, an amount, and the like of the porous material.

According to an embodiment, a temperature difference △T1 between ageometric center formed by adjacent bars 31 and a point at which each ofthe bars 31 is located may be preferably provided to be less than 0.5°C. Also, a temperature difference △T2 between the geometric centerformed by the adjacent bars 31 and an edge portion of the vacuumadiabatic body may be preferably provided to be less than 0.5° C. In thesecond plate member 20, a temperature difference between an averagetemperature of the second plate and a temperature at a point at which aheat transfer path passing through the conductive resistance sheet 60 or63 meets the second plate may be the largest. For example, when thesecond space is a region hotter than the first space, the temperature atthe point at which the heat transfer path passing through the conductiveresistance sheet meets the second plate member becomes the lowest.Similarly, when the second space is a region colder than the firstspace, the temperature at the point at which the heat transfer pathpassing through the conductive resistance sheet meets the second platemember becomes the highest.

This means that the amount of heat transferred through other pointsexcept the surface conduction heat passing through the conductiveresistance sheet should be controlled, and the entire heat transferamount satisfying the vacuum adiabatic body may be achieved only whenthe surface conduction heat occupies the largest heat transfer amount.To this end, a temperature variation of the conductive resistance sheetmay be controlled to be larger than that of the plate member.

Physical characteristics of the parts constituting the vacuum adiabaticbody will be described. In the vacuum adiabatic body, a force by vacuumpressure is applied to all of the parts. Therefore, a material having astrength (N/m2) of a certain level may be preferably used.

Under such circumferences, the plate members 10 and 20 and the sideframe 70 may be preferably made of a material having a sufficientstrength with which they are not damaged by even vacuum pressure. Forexample, when the number of bars 31 is decreased so as to limit thesupport conduction heat, deformation of the plate member occurs due tothe vacuum pressure, which may bad influence on the external appearanceof refrigerator. The radiation resistance sheet 32 may be preferablymade of a material that has a low emissivity and may be easily subjectedto thin film processing. Also, the radiation resistance sheet 32 is toensure a strength enough not to be deformed by an external impact. Thesupporting unit 30 is provided with a strength enough to support theforce by the vacuum pressure and endure an external impact, and is tohave machinability. The conductive resistance sheet 60 may be preferablymade of a material that has a thin plate shape and may endure the vacuumpressure.

In an embodiment, the plate member, the side frame, and the conductiveresistance sheet may be made of stainless materials having the samestrength. The radiation resistance sheet may be made of aluminum havinga weaker strength that the stainless materials. The supporting unit maybe made of resin having a weaker strength than the aluminum.

Unlike the strength from the point of view of materials, analysis fromthe point of view of stiffness is required. The stiffness (N/m) is aproperty that would not be easily deformed. Although the same materialis used, its stiffness may be changed depending on its shape. Theconductive resistance sheets 60 or 63 may be made of a material having astrength, but the stiffness of the material is preferably low so as toincrease heat resistance and minimize radiation heat as the conductiveresistance sheet is uniformly spread without any roughness when thevacuum pressure is applied. The radiation resistance sheet 32 requires astiffness of a certain level so as not to contact another part due todeformation. Particularly, an edge portion of the radiation resistancesheet may generate conduction heat due to drooping caused by theself-load of the radiation resistance sheet. Therefore, a stiffness of acertain level is required. The supporting unit 30 requires a stiffnessenough to endure a compressive stress from the plate member and anexternal impact.

In an embodiment, the plate member and the side frame may preferablyhave the highest stiffness so as to prevent deformation caused by thevacuum pressure. The supporting unit, particularly, the bar maypreferably have the second highest stiffness. The radiation resistancesheet may preferably have a stiffness that is lower than that of thesupporting unit but higher than that of the conductive resistance sheet.Lastly, the conductive resistance sheet may be preferably made of amaterial that is easily deformed by the vacuum pressure and has thelowest stiffness.

Even when the porous material 33 is filled in the vacuum space part 50,the conductive resistance sheet may preferably have the loweststiffness, and the plate member and the side frame may preferably havethe highest stiffness.

Hereinafter, a vacuum pressure preferably determined depending on aninternal state of the vacuum adiabatic body. As already described above,a vacuum pressure is to be maintained inside the vacuum adiabatic bodyso as to reduce heat transfer. At this time, it will be easily expectedthat the vacuum pressure is preferably maintained as low as possible soas to reduce the heat transfer.

The vacuum space part may resist to heat transfer by only the supportingunit 30. Here, a porous material 33 may be filled with the supportingunit inside the vacuum space part 50 to resist to the heat transfer. Theheat transfer to the porous material may resist without applying thesupporting unit.

The case where only the supporting unit is applied will be described.

FIG. 5 illustrates graphs showing changes in adiabatic performance andchanges in gas conductivity with respect to vacuum pressures by applyinga simulation.

Referring to FIG. 5 , it may be seen that, as the vacuum pressure isdecreased, i.e., as the vacuum degree is increased, a heat load in thecase of only the main body (Graph 1) or in the case where the main bodyand the door are joined together (Graph 2) is decreased as compared withthat in the case of the typical product formed by foaming polyurethane,thereby improving the adiabatic performance. However, it may be seenthat the degree of improvement of the adiabatic performance is graduallylowered. Also, it may be seen that, as the vacuum pressure is decreased,the gas conductivity (Graph 3) is decreased. However, it may be seenthat, although the vacuum pressure is decreased, the ratio at which theadiabatic performance and the gas conductivity are improved is graduallylowered. Therefore, it is preferable that the vacuum pressure isdecreased as low as possible. However, it takes long time to obtainexcessive vacuum pressure, and much cost is consumed due to excessiveuse of a getter. In the embodiment, an optimal vacuum pressure isproposed from the above-described point of view.

FIG. 6 is a graph illustrating results obtained by observing a time anda pressure in a process of exhausting the inside of the vacuum adiabaticbody when a supporting unit is used.

Referring to FIG. 6 , in order to create the vacuum space part 50 to bein the vacuum state, a gas in the vacuum space part 50 is exhausted by avacuum pump while evaporating a latent gas remaining in the parts of thevacuum space part 50 through baking. However, if the vacuum pressurereaches a certain level or more, there exists a point at which the levelof the vacuum pressure is not increased any more (△T1). After that, thegetter is activated by disconnecting the vacuum space part 50 from thevacuum pump and applying heat to the vacuum space part 50 (△T2). If thegetter is activated, the pressure in the vacuum space part 50 isdecreased for a certain period of time, but then normalized to maintaina vacuum pressure of a certain level. The vacuum pressure that maintainsthe certain level after the activation of the getter is approximately1.8×10-6 Torr.

In the embodiment, a point at which the vacuum pressure is notsubstantially decreased any more even though the gas is exhausted byoperating the vacuum pump is set to the lowest limit of the vacuumpressure used in the vacuum adiabatic body, thereby setting the minimuminternal pressure of the vacuum space part 50 to 1.8×10-6 Torr.

FIG. 7 is a graph obtained by comparing a vacuum pressure with gasconductivity.

Referring to FIG. 7 , gas conductivities with respect to vacuumpressures depending on sizes of a gap in the vacuum space part 50 arerepresented as graphs of effective heat transfer coefficients (eK).Effective heat transfer coefficients (eK) were measured when the gap inthe vacuum space part 50 has three sizes of 2.76 mm, 6.5 mm, and 12.5mm. The gap in the vacuum space part 50 is defined as follows. When theradiation resistance sheet 32 exists inside vacuum space part 50, thegap is a distance between the radiation resistance sheet 32 and theplate member adjacent thereto. When the radiation resistance sheet 32does not exist inside vacuum space part 50, the gap is a distancebetween the first and second plate members.

It was seen that, since the size of the gap is small at a pointcorresponding to a typical effective heat transfer coefficient of 0.0196W/mK, which is provided to a adiabatic material formed by foamingpolyurethane, the vacuum pressure is 2.65×10-1 Torr even when the sizeof the gap is 2.76 mm. Meanwhile, it was seen that the point at whichreduction in adiabatic effect caused by gas conduction heat is saturatedeven though the vacuum pressure is decreased is a point at which thevacuum pressure is approximately 4.5×10-3 Torr. The vacuum pressure of4.5×10-3 Torr may be defined as the point at which the reduction inadiabatic effect caused by gas conduction heat is saturated. Also, whenthe effective heat transfer coefficient is 0.1 W/mK, the vacuum pressureis 1.2×10-2 Torr.

When the vacuum space part 50 is not provided with the supporting unitbut provided with the porous material, the size of the gap ranges from afew micrometers to a few hundreds of micrometers. In this case, theamount of radiation heat transfer is small due to the porous materialeven when the vacuum pressure is relatively high, i.e., when the vacuumdegree is low. Therefore, an appropriate vacuum pump is used to adjustthe vacuum pressure. The vacuum pressure appropriate to thecorresponding vacuum pump is approximately 2.0×10-4 Torr. Also, thevacuum pressure at the point at which the reduction in adiabatic effectcaused by gas conduction heat is saturated is approximately 4.7×10-2Torr. Also, the pressure where the reduction in adiabatic effect causedby gas conduction heat reaches the typical effective heat transfercoefficient of 0.0196 W/mK is 730 Torr.

When the supporting unit and the porous material are provided togetherin the vacuum space part, a vacuum pressure may be created and used,which is middle between the vacuum pressure when only the supportingunit is used and the vacuum pressure when only the porous material isused. When only the porous material is used, the lowest vacuum pressuremay be used.

FIG. 8 is a cross-sectional perspective view of an edge of the vacuumadiabatic body.

Referring to FIG. 8 , a first plate member 10, a second plate member 20,and a conductive resistance sheet 60 are provided. The conductiveresistance sheet 60 may be provided as a thin plate to resist to thermalconduction between the plate members 10 and 20. Although the conductiveresistance sheet 60 is provided as a flat plan shape as a thin plate,the conductive resistance sheet 60 may have a curved shape by beingpulled inward when vacuum is applied to the vacuum space part 50.

Since the conductive resistance sheet 60 has the thin plate shape andlow strength, the conductive resistance sheet 60 may be damaged by evenan external small impact. As a result, when the conductive resistancesheet 60 is damaged, the vacuum of the vacuum space part may be broken,and thus, performance of the vacuum adiabatic body may not be properlyexerted. To solve this limitation, a sealing frame 200 may be disposedon an outer surface of the conductive resistance sheet 60. According tothe sealing frame 200, components of the door 3 or other components maynot directly contact the conductive resistance sheet 60 but indirectlycontact the conductive resistance sheet 60 through the sealing frame 200to prevent the conductive resistance sheet 60 from being damaged. Toallow the sealing frame 200 to prevent an impact from being applied tothe conductive resistance sheet 60, the two members may be spaced apartfrom each other, and a buffer member may be interposed between the twomembers.

To reinforce the strength of the vacuum adiabatic body, a reinforcementmember may be provided on each of the plate members 10 and 20. Forexample, the reinforcement member may include a first reinforcementmember 100 coupled to an edge portion of the second plate member 10 anda second reinforcement member 110 coupled to an edge portion of thefirst plate member 10. To improve the strength of the vacuum adiabaticbody, a member having a thickness and strength greater than those of theplate member 10 may be applied to the reinforcement members 100 and 110.The first reinforcement member 100 may be provided in an internal spaceof the vacuum space part 50, and the second reinforcement member 110 maybe provided on an inner surface part of the main body 2.

The conductive resistance sheet 60 may not contact the reinforcementmembers 100 and 110. This is done because thermal conductive resistancecharacteristics generated in the conductive resistance sheet 60 isdestroyed by the reinforcement members. That is to say, a width of anarrow heat bridge (heat bridge) that resists to the thermal conductionis greatly expanded by the reinforcement member, and the narrow heatbridge characteristics are destroyed.

Since the width of the internal space of the vacuum space part 50 isnarrow, the first reinforcement member 100 may be provided in a flatplate shape in cross-section. The second reinforcement member 110provided on the inner surface of the main body 2 may be provided in ashape of which a cross-section is bent.

The sealing frame 200 may include an inner surface part 230 disposed inthe internal space of the main body 2 and supported by the first platemember 10, an outer surface part 210 disposed in the external space ofthe main body 2 and supported by the second plate member 20, and a sidesurface part 220 disposed on a side surface of the edge of the vacuumadiabatic body constituting the main body 2 to cover the conductiveresistance sheet 60 and connect the inner surface part 230 to the outersurface part 210.

The sealing frame 200 may be made of a resin material that is slightlydeformable. A mounted position of the sealing frame 200 may bemaintained by an interaction between the inner surface part 230 and theouter surface part 210, i.e., by a holding action. That is to say, theset position may not be separated.

The position fixing of the sealing frame 200 will be described indetail.

First, movement of the plate members 10 and 20 in the extensiondirection (a y-axis direction in FIG. 8 ) on the plane may be fixed bybeing supported by the inner surface part 230 by being hooked on thesecond reinforcement member 110. In more detail, the sealing frame 200may move out of the vacuum adiabatic body by interfering with the innersurface part 230 of the second reinforcement member 110. On the otherhand, the movement of the sealing frame 200 to the inside of the vacuumadiabatic body may be interrupted by at least one action of first actionin which the inner surface part 230 is hooked to be supported by thesecond reinforcement member 110 (this action may act in both directionsin addition to elastic restoring force of the sealing frame made of aresin), second action in which the side surface part 220 is stopped withrespect to the plate member 10, and third action in which the innersurface part 230 prevents the first plate member 10 from moving in they-axis direction.

The movement of the sealing frame 200 in the vertical extensiondirection (an x-axis direction in FIG. 8 ) with respect to thecross-section of the plate members 10 and 20 may be fixed by hooking andsupporting the outer surface part 210 to the second plate member 20. Inthe auxiliary action, the movement of the sealing frame 200 in thex-axis direction may be interrupted by the action of hooking the secondreinforcement member 110 and the folding action.

The movement of the sealing frame 200 in the extension direction (az-axis direction in FIG. 8 ) may be stopped by at least one of firstaction in which the inner surface part 230 of one sealing frame 200contacts the inner surface of the other sealing frame 200 and secondaction in which the inner surface part 230 of one sealing frame 200contacts a mullion 300.

FIGS. 9 and 10 are schematic views of the main body when viewed from thefront side. In the drawings, it should be noted that the sealing frame200 shows a virtual state in which the inner surface part 230 is spreadin a direction parallel to the side surface part 220.

Referring to FIGS. 9 and 10 , the sealing frame 200 may include members200 b and 200 e that respectively seal upper and lower edges of the mainbody 2. The side edge of the main body 2 may be divided according towhether the spaces within the refrigerator, which are divided on thebasis of the mullion 300, are separately (in FIG. 9 ) or integrally (inFIG. 10 ) sealed.

When the side edge of the main body 2 is separated as shown in FIG. 9 ,it may be divided into four sealing frames 200 a, 200 c, 200 d and 200f. When the side edge of the main body 2 is integrally sealed as shownin FIG. 10 , it may be divided into two sealing frames 200 g and 200 c.

When the side edge of the main body 2 is sealed with the two sealingframes 200 g and 200 c as shown in FIG. 10 , since two couplingoperations may be required, the manufacturing may be facilitated.However, it is necessary to cope with such a limitation because there isa risk of a loss of cold air.

In the case of sealing the side edge of the main body 2 with the foursealing frames 200 a, 200 c, 200 d and 200 f as shown in FIG. 9 , fourcoupling operations may be required, and thus, the manufacturing may beinconvenient. However, the thermal conduction may be interrupted toreduce the heat transfer between the separated storage rooms, therebyreducing the loss of the cold air.

The embodiment of the vacuum adiabatic body shown in FIG. 8 may bepreferably exemplify the vacuum adiabatic body on the main body.However, it does not exclude that it is provided to the door-side vacuumadiabatic body. Since a gasket is installed on the door 3, the sealingframe 200 may be disposed on the main body-side vacuum adiabatic body.In this case, the side surface part 220 of the sealing frame 200 mayfurther have the advantage that the gasket provides a sufficient widthfor the contact.

In more detail, since the width of the side surface part 220 is widerthan the adiabatic thickness of the vacuum adiabatic body, that is, thewidth of the vacuum adiabatic body, an adiabatic width of the gasket maybe provided at a sufficiently wide width. For example, when theadiabatic thickness of the vacuum adiabatic body is about 10 mm, thereis an advantage that the storage space of the refrigerator is enlargedby providing a large storage space in the cavity. However, there is aproblem that the gap of about 10 mm does not provide a sufficient gapfor the contact of the gasket. In this case, since the side surface part220 provides a wide gap corresponding to the contact area of the gasket,it is possible to effectively prevent the cold air from being lostthrough the contact interval between the main body 2 and the door 3.That is, when the contact width of the gasket is about 20 mm, eventhough the width of the side surface part 220 may be about 20 mm ormore, the side surface part 220 may have a width about 20 mm or more tocorresponding to the contact width of the gasket.

It may be understood that the sealing frame 200 performs the shieldingof the conductive resistance sheet and the sealing function to preventthe cold air from being lost.

FIG. 11 is a cross-sectional view of a contact part in a state in whichthe main body is closed by the door.

Referring to FIG. 11 , the gasket 80 is disposed between the main body 2and the door 3. The gasket 80 may be coupled to the door 3 and providedas a member that is made of a soft deformable material. The gasket 80includes a magnet as one component. When the magnet approaches bypulling a magnetic body (i.e., a magnetic body of an edge portion of themain body), a contact surface between the main body 2 and the door 3 maybe blocked by the sealing surface having a predetermined width due tothe smooth deformation of the gasket 80.

In detail, when a gasket sealing surface 81 of the gasket contacts theside surface part 220, a sealing surface 221 of the side surface parthaving a sufficient width may be provided. The sealing surface 221 ofthe side surface part may be defined as a contact surface on the sidesurface part 220 which is in contact with the gasket sealing surface 81when the gasket 80 contacts the side surface part 220.

Thus, it is possible to secure the sealing surfaces 81 and 221 having asufficient area irrespective of the adiabatic thickness of the vacuumadiabatic body. This is because even if the adiabatic thickness of thevacuum adiabatic body is narrow, and the adiabatic thickness of thevacuum adiabatic body is narrower than the gasket sealing surface 81, ifthe width of the side surface part 220 increases, the sealing surface221 of the side surface part having the sufficient width may beobtained. In addition, the sealing surfaces 81 and 221 having thesufficient area may be ensured irrespective of the deformation of themember, which may affect the deformation of the contact surface betweenthe main body and the door. This is because it is possible to provide apredetermined clearance in and out of the side surface sealing surface221 in designing the side surface part 220 so that even if the slightdeformation occurs between the sealing surfaces 81 and 221, the widthand area may be maintained.

In the sealing frame 200, the outer surface part 210, the side surfacepart 220, and the inner surface part 230 may be provided, and their setpositions may be maintained. Briefly, the outer surface part 210 and theinner surface part 230 may be provided in a shape, i.e., a recessedgroove shape that is capable of holding end portion of the vacuumadiabatic body, more particularly, the plate members 10 and 20. Here, itmay be understood that the recessed groove has a configuration of arecessed groove as a constitution in which a width between the endportions of the outer surface part 210 and the inner surface part 230 isless than the width of the side surface part 220.

The coupling of the sealing frame 200 will be briefly described. First,the side surface part 220 and the outer surface part 210 rotate in thedirection of the second plate member 20 in a state in which the innersurface part 230 is hooked with the second reinforcement member 110.Thus, the sealing frame 200 is elastically deformed, and the outersurface part 210 may move inward along the outer surface of the secondplate member 20 to complete the coupling. When the coupling of thesealing frame is completed, the sealing frame may return to its originalshape before being deformed. When the coupling is completed, theinstallation position may be maintained as described above.

Detailed configuration and operation of the sealing frame 200 will bedescribed.

The outer surface part 210 is provided with an extension part 211 thatextends to the outside of the refrigerator (hereinafter, referred to asan outward extension part), which extends inward from an end of thesecond plate member 20 and a contact part 212 outside the refrigerator(hereinafter, referred to as an outside contact part), which contactsthe outer surface of the second plate member 20 at an end of the outsideextension part 211.

The outward extension part 211 may have a predetermined length toprevent the outer surface part 210 from being separated by external weakforce. That is to say, even though the outer surface part 210 is forcedto be pulled toward the door due to carelessness of the user, the outersurface part 210 may not be completely separated from the second platemember 20. However, if it is excessively long, there is difficulty inintentional removal at the time of repair, and it is preferable that thelength is limited to a predetermined length because the couplingoperation becomes difficult.

The outside contact portion 212 may be provided with a structure inwhich an end of the outside extension part 211 is slightly bent towardthe outer surface of the second plate member 20. Thus, the sealing dueto the contact between the outer surface part 210 and the second platemember 20 may be completed to prevent foreign substances from beingintroduced.

The side surface part 220 is bent at an angle of about 90 degrees fromthe outer surface part 210 toward the opening of the main body 2 and isprovided with a width enough to secure the sufficient width of the sidesurface sealing surface 221. The side surface part 220 may be providedthinner than the inner surface part 210 and the outer surface part 230.This is for the purpose of permitting the elastic deformation at thetime of coupling or removing the sealing frame 200 and the purpose ofnot permitting a distance to cause magnetic force between the magnetdisposed on the gasket 80 and the magnetic body on the side of the bodyso that the magnetic force is weakened. The side surface part 220 mayhave a purpose of protecting the conductive resistance sheet 60 andarranging an outer appearance as an exposed portion of the outside. Whenthe adiabatic member is provided inside the side surface part 220, theadiabatic performance of the conductive resistance sheet 60 may bereinforced.

The inner surface part 230 extends from the side surface part 220 in thedirection of the inside of the refrigerator, that is, in the rearsurface direction of the main body, at about 90 degrees. The innersurface part 230 may perform an action for fixing the sealing frame 200,an operation for installing components that is necessary for operationof a product to which the vacuum adiabatic body is installed, such as arefrigerator, and an operation for preventing an external inflow offoreign substances.

The operation corresponding to each constituent of the inner surfacepart 230 will be described.

The inner surface part 230 is provided with an extension part 231 thatextends to inside of the refrigerator (hereinafter, referred to as aninward extension part), which is bent from an inner end of the sidesurface part 220 to extend and a first member coupling part 232 bentfrom an inner end of the inward extension part 231, i.e., toward theinner surface of the first plate member 10. The first member couplingpart 232 may contact a protrusion part 112 of the second reinforcementpart 110 so as to be hooked. The inward extension part 231 may providean interval extending toward the inside of the refrigerator so that thefirst member coupling part 232 is hooked with the inside of the secondreinforcement member 110.

Since the first member coupling part 232 is hooked with the secondreinforcement member 110, the supporting operation of the sealing frame200 may be realized. The second reinforcement member 110 may furtherinclude a base part 111 coupled to the first plate member 10 and aprotrusion part 112 bent and extending from the base part 111. Aninertia moment of the second reinforcement member 110 may increase by astructure of the base part 111 and the protruding part 112 so thatability to resist the bending strength increases.

The first member coupling part 232 and the second member coupling part233 may be coupled to each other. The first and second member couplingparts 232 and 233 may be provided as separate members to be coupled toeach other or may be provided as a single member from the design stage.

A gas formation part 234 that further extends from the inner end of thesecond member coupling part 233 to the inside of the refrigerator may befurther provided. The gap formation part 234 may serve as a portion forproviding a space or a space in which components necessary for operationof the appliance such as the refrigerator provided with the vacuumadiabatic body are disposed.

An inclined part 235 that is inclined to the inside of the refrigerator(hereinafter, referred to as an inward inclined part) is furtherprovided. The inward inclined part 235 may be provided so as to beinclined toward the end, that is, toward the first plate member 10toward the inside of the refrigerator. The inward inclined part 235 maybe provided so that a gap between the sealing frame and the first platemember becomes smaller inward. Thus, it is possible to secure a spacefor mounting a component such as a lamp by cooperation with the gapforming portion 234 while minimizing the volume occupying the internalspace of the sealing frame 200 as much as possible.

An inside contact part 236 is disposed on an inner end of the inwardinclined part 235. The inside contact portion 236 may be provided with astructure in which an end of the inward inclined part 235 is slightlybent toward the inner surface of the second plate member 10. Thus, thesealing due to the contact between the inner surface part 230 and thesecond plate member 10 may be completed to prevent foreign substancesfrom being introduced.

When an accessory part such as a lamp is installed on the inner surfacepart 230, the inner surface part 230 may be divided into two parts toachieve the purpose of the installation convenience of the part. Forexample, the inner surface part 230 may be divided into a first memberfor providing the inward extending portion 231 and the first membercoupling part 232 and a second member providing the second membercoupling part 233, the gap formation part 234, the inward inclined part235, and inside contact part 236. In a state in which an product such asthe lamp is mounted on the second member, the first member and thesecond member may be coupled to each other in such a manner that thesecond member coupling part 233 is coupled to the first member couplingpart 232. Alternatively, it does not exclude that the inner surface part230 is provided in more various manners. For example, the inner surfacepart 230 may be provided as a single member.

FIG. 12 is a cross-sectional view illustrating a contact part of a mainbody and a door according to another embodiment. This embodiment ischaracteristically different in the position of the conductiveresistance sheet and accordingly the change of other portions.

Referring to FIG. 12 , in this embodiment, the conductive resistancesheet 60 may be provided inside the refrigerator, but not provided onthe edge portion of the end of the vacuum adiabatic body. The secondplate member 20 may extend over the outside of the refrigerator and theedge portion of the vacuum adiabatic body. In some cases, the secondplate member 20 may extend by a predetermined length up to the inside ofthe refrigerator. In this embodiment, It may be seen that a conductiveresistance sheet is provided at a position similar to the conductiveresistance sheet of the door-side vacuum adiabatic body shown in FIG. 4b .

In this case, the second reinforcement member 110 may move to the insideof the refrigerator without contacting the conductive resistance sheet60 in order not to affect the high thermal conductive adiabaticperformance of the conductive resistance sheet 60. This is done forachieving a function of a heat bridge of the conductive resistancesheet. Thus, the conductive resistance sheet 60 and the secondreinforcement member 110 do not contact each other so that theconductive adiabatic performance by the conductive resistance sheet andthe strength reinforcement performance of the vacuum adiabatic body bythe reinforcement member are achieved at the same time.

In this embodiment, it may be applied to the case in which perfectthermal protection and physical protection for the edge portion of thevacuum adiabatic body are required.

FIGS. 13 and 14 are partial cutaway perspective views illustrating thecoupling of the two members in the embodiment in which the inner surfacepart is divided into two members, wherein FIG. 13 is a state in whichthe coupling is completed, and FIG. 14 is a view illustrating thecoupling process.

Referring to FIGS. 13 and 14 , a first member coupling part 232 ishooked with a protrusion part 112 of a second reinforcement member 110,and an outer surface part 210 is supported by a second plate member 20.Thus, a sealing frame 200 may be fixed to an edge portion of the vacuumadiabatic body.

At least one or more first member insertion parts 237 that is bent toextend to the inside of the refrigerator may be provided at end portionsof the first member coupling part 232. For example, at least one or morefirst member insertion parts 237 may be provided for each sealing frame200 installed in the refrigerator. A second member insertion recess 238may be provided in a position corresponding to the first memberinsertion part 237. The first member insertion part 237 and the secondmember insertion recess 238 may be similar in size and shape to eachother. Thus, the first member insertion part 237 may be inserted intothe second member insertion recess 238 and then be fitted and fixed.

The coupling of the first member and the second member will bedescribed. In the state in which the first member is coupled to the edgeof the vacuum adiabatic body, the second member may be aligned withrespect to the first member so that the second member insertion recess238 corresponds to the first member insertion part 237. When the firstmember insertion part 237 is inserted into the second member insertionrecess 238, the two members may be coupled to each other.

To prevent the coupled second member from being separated from the firstmember, at least a portion of the second member insertion recess 238 mayhave a size less than that of the first member insertion part 237. Thus,the two members may be forcibly fitted. To perform an action of beinghooked and supported after the second member insertion recess 238 andthe first member insertion part 237 are inserted by a predetermineddepth, a protrusion and a groove may be respectively provided on/in anypoint after the predetermined depth. Here, after the two members areinserted at a certain depth, the two members may be inserted furtherbeyond the jaws to allow the two members to be more firmly fixed. Here,the worker may feel that he/she is correctly inserted through thefeeling.

The two members constituting the inner surface part may be fixed at theposition and the coupling relation by the structure in which the twomember are inserted and coupled to each other. Alternatively, when aload is large due to the action of the second member that fixes aseparator component, the first member and the second member may becoupled to each other by a separate coupling member such as an innercoupling tool 239.

FIG. 15 is a view for sequentially explaining coupling of the sealingframe when the sealing frame is provided as two members according to anembodiment. Particularly, a case in which a component is installed onthe inner surface part will be described as an example.

Referring to FIG. 15(a), the sealing frame 200 is coupled to the edgeportion of the vacuum adiabatic body. Here, the coupling may beperformed by using elastic deformation of the sealing frame 200 andrestoring force due to the elastic deformation without a separate membersuch as a screw.

For example, in the state in which the inner surface part 230 is hookedwith the second reinforcement member 110, the side surface part 220 andthe outer surface part 210 rotate in the direction of the second platemember 20 by using a connection point between the inner surface part 230and the side surface part 220 as a rotation center. This action maycause elastic deformation of the side surface part 220.

Thereafter, the outer surface part 210 may move inward from the outersurface of the second plate member 20 so that the elastic force of theside surface part 220 acts on the outer surface part 210 and thuslightly coupled. When the coupling of the sealing frame is completed,the sealing frame may be seated in its original position designed in itsoriginal shape designed.

Referring to FIG. 15(b), a state in which the first member of thesealing frame 200 is completely coupled is shown. The side surface part220 may be formed with a thin thickness when compared to that of each ofthe outer surface part 210 and the inner surface part 230 so that thesealing frame 200 is coupled to the edge of the vacuum adiabatic body bythe elastic deformation and the elastic restoring action of the sealingframe.

Referring to FIG. 15(c), a component seating member 250 as a separatecomponent is provided as the second member providing the inner surfacepart 230. The component seating member 250 may be a component on whichthe component 399 is placed so that its set position is supported, andan additional function that is necessary for the operation of thecomponent 399 may be further performed. For example, in this embodiment,when the component 399 is the lamp, the gap formation part 234 made of atransparent member may be disposed on the component seating member 250.Thus, light irradiated from the lamp may pass through the inner surfacepart 230 and be irradiated into the refrigerator, and the user mayidentify the article in the refrigerator.

The component seating member 250 may have a predetermined shape that iscapable of being fitted with the component 399 to fix a position of thecomponent 399.

FIG. 15(d) illustrates a state in which the component 399 is paced onthe component seating member 250.

Referring to FIG. 15(e), the component seating member 250 on which thecomponent 399 is seated is aligned in a predetermined direction so as tobe coupled to the first member providing the inner surface part. In thisembodiment, the first member coupling part 232 and the second memberinsertion recess 238 may be aligned with each other in the extensiondirection so that the first member coupling part 232 is inserted intothe second member insertion recess 238. Alternatively, although notlimited in this way, it may be advantageously proposed to enhance theease of assembly.

To allow the first member coupling part 232 and the second memberinsertion recess 238 to be forcibly fitted with respect to each other,the first member coupling part 232 may be slightly larger than thesecond member insertion recess 238 and have a hook structure such as aprotrusion and a projection so as to realize easy insertion.

Referring to FIG. 15(f), the inner surface part in a completelyassembled state is illustrated.

FIGS. 16 and 17 are views illustrating one end portion of the sealingframe, wherein FIG. 16 illustrates a state before a door hinge isinstalled, and FIG. 17 illustrates a state in which the door hinge isinstalled.

In the case of the refrigerator, a door hinge is provided at theconnection part so that the door-side vacuum adiabatic body is rotatablycoupled to the main body-side adiabatic body. The door hinge has to havepredetermined strength and also be capable of preventing drooping of thedoor due to its own weight in a state in which the door is coupled andpreventing the main body from being twisted.

Referring to FIG. 16 , to couple the door hinge 263, a door couplingtool 260 is provided on the main body-side vacuum adiabatic body. Thedoor coupling tool 260 may be provided in three. The door coupling tool260 may be directly or indirectly fixed to the second plate member 20and/or the reinforcement members 100 and 110 and/or a separateadditional reinforcement member (for example, an additional platefurther provided on the outer surface of the second plate member). Here,the expression ‘direct’ may be referred to as a fusing method such aswelding, and the expression ‘indirect’ may refer to a coupling methodusing an auxiliary coupling tool or the like instead of the fusion orthe like.

Since the door coupling tool 260 requires high supporting strength, thedoor coupling tool 260 may be coupled to the second plate member 20. Forthis, the sealing frame 200 may be cut, and the sealing frame 200 to becut may be the upper sealing frame 200 b at an upper edge of the mainbody-side vacuum adiabatic body. Also, the sealing frame 200 may includeright sealing frames 200 a, 200 f, and 200 g on a right edge of the mainbody-side vacuum adiabatic body, and a lower side sealing frame 200 e ona lower edge of the main body-side vacuum adiabatic body. If the doorinstallation direction is different, the left sealing frames 200 a, 200f, and 200 g at the left edge of the body-side vacuum adiabatic body maybe used.

The sealing frame 200 to be cut may have a cutoff surface 261, and thesecond plate member 20 may have a door coupling tool seating surface 262to which the door coupling tool 260 is coupled. Thus, the sealing frame220 may be cut to be exposed to the outside of the door coupling toolseating surface 262, and an additional plate member may be furtherinserted into the door coupling tool seating surface 262.

As described in the drawings, the end portion of the sealing frame 200may not be entirely removed, but a portion of the sealing frame 200 maybe removed only at a portion at which the door coupling tool 260 isprovided. However, it may be more preferable that all the end portionsof the sealing frame 200 are removed to facilitate the manufacture andto allow the door hinge 263 to contact the vacuum adiabatic body so asto be firmly coupled to the vacuum adiabatic body.

FIG. 18 is a view for explaining an effect of the sealing frameaccording to an embodiment in comparison with the technique according tothe related art, wherein FIG. 18(a) is a cross-sectional view of thecontact part of the main body-side vacuum adiabatic body and the dooraccording to an embodiment, and FIG. 18(b) is a cross-sectional view ofthe main body and the door according to the related art.

Referring to FIG. 18 , in the refrigerator, a hot line may be providedat the contact portion between the door and the main body to prevent dewformation due to sharp temperature change. As the hot line is closer tothe outer surface and the edge of the main body, the dew condensationmay be removed even with small heat capacity.

According to an embodiment, the hot line 270 may be disposed in aninternal space of a gap between the second plate member 20 and thesealing frame 200. A hot line accommodation part 271 in which the hotline 270 is disposed may be further provided in the sealing frame 200.Since the hot line 270 is placed outside the conductive resistance sheet60, an amount of heat transferred to the inside of the refrigerator issmall. Thus, the dew condensation on the main body and the door contactpart may be prevented by using smaller heat capacity. In addition, thehot line 270 may be disposed on a relative outside of the refrigerator,i.e., a bent portion between the edge of the main body and the outersurface of the main body to prevent heat from being introduced into theinternal space of the refrigerator.

In this embodiment, the side surface part 220 of the sealing frame 200may have a portion w1 that is aligned with the gasket 80 and the vacuumspace part 50 and a portion w2 that is not aligned with the vacuum spacepart 50 but aligned with the gasket 80 and the internal space of therefrigerator. This is a portion provided by the side surface part 220 toensure sufficient cold air interruption by the magnet. Thus, the sealingeffect by the gasket 80 may be sufficiently achieved by the sealingframe 200.

In this embodiment, the inward inclined part 235 is provided to beinclined toward the inner surface of the first plate member 10 at apredetermined angle β. This makes it possible to give the effect inwhich the capacity within the refrigerator increases so that the narrowspace within the refrigerator is more widely used. That is to say, likethe related art, the inward inclined part may be inclined to a directionopposite to the predetermined angle β toward the internal space of therefrigerator to widely utilize a space that is close to the door. Forexample, more foods may be accommodated in the door, and more space foraccommodating various components that are necessary for operation of thedevice may be defined.

Hereinafter, various embodiments in which the sealing frame 200 isinstalled will be described with reference to FIGS. 19 to 24 .

Referring to FIG. 19 , the second reinforcement member 110 may includeonly a base part 111 but do not include a protrusion part 112. In thiscase, a groove 275 may be provided in the base part 111. An end portionof the first member coupling part 232 may be inserted into the groove275. In this embodiment, it may be applied in a case of an article whichprovides sufficient strength without providing the protrusion part 112on the second reinforcement member 110.

In this embodiment, the sealing frame 200 may be coupled to the endportion of the vacuum adiabatic body by aligning the first membercoupling part 232 to be inserted into the groove 275 when the sealingframe 200 is coupled.

According to the coupling action of the groove 275 and the first membercoupling part 232, the movement of the sealing frame 200 in the y-axisdirection may be stopped through only the coupling of the inner surfacepart 230 of the sealing frame 200 and the second reinforcement part 110.

Referring to FIG. 20 , the this embodiment is different from theabove-described embodiment of FIG. 19 except that the base part 111 isfurther provided with a reinforcement base part 276. A groove 277 may befurther provided in the reinforcement base part 276 so that an endportion of the first member coupling part 232 is inserted. In thisembodiment, even though the second reinforcement member 110 is notprovided with the protrusion part 112 because of an insufficient spaceor interference with the installation space, it may be applied when itis necessary to reinforce the strength to a predetermined level. That isto say, it may be applied when the strength reinforcement of the mainbody-side vacuum adiabatic body is provided at a level of strengthreinforcement which is obtained by further providing a reinforcementbase 276 at the outer end of the base part 111.

A groove 277 is provided in the reinforcement base part 276, and an endportion of the first member coupling part 232 is inserted into thegroove part 277 to align the sealing frame 200 with the vacuum adiabaticbody. Thus, the sealing frame 200 may be coupled to the end portion ofthe vacuum adiabatic body.

According to the coupling action of the groove 277 and the first membercoupling part 232, the movement of the sealing frame 200 in the y-axisdirection may be stopped through only the coupling of the inner surfacepart 230 of the sealing frame 200 and the second reinforcement part 110.

Referring to FIG. 21 , the this embodiment is different from theabove-described embodiment of FIG. 19 except that the base part 111 isfurther provided with a reinforcement protrusion 278. The end portion ofthe first member coupling part 232 may be hooked on the reinforcementprotrusion 278. In this embodiment, even though the second reinforcementmember 110 is not provided with the protrusion part 112 or thereinforcement base part 276 because of an insufficient space orinterference with the installation space, it may be applied when it isnecessary to reinforce the strength to a predetermined level and toallow the first member coupling part 232 to be hooked. That is to say,the reinforcement protrusion 278 may be further disposed on an outer endportion of the base part 111 to obtain a strength reinforcement effectof the main body-side vacuum adiabatic body. Also, the reinforcementprotrusion 278 may be applied because it provides a hook action of thefirst member coupling part 232.

The first member coupling part 232 may be hooked to be supported by thereinforcement protrusion 278 so that the sealing frame 200 is coupled tothe end portion of the vacuum adiabatic body.

The embodiment proposed in FIGS. 19 to 21 illustrates a case in whichthe inner surface part 230 is not dived into the first member and thesecond member but is provided as a single product to be coupled to thevacuum adiabatic body. However, this embodiment is not limited thereto.For example, the sealing frame 200 may be divided into the two members.

Although the second reinforcement member 110 is provided in the aboveembodiment, a case in which the sealing frame 200 is coupled when aseparate reinforcement member is not provided inside the first platemember 10 will be described in the following embodiment.

Referring to FIG. 22 , although the first reinforcement member 100 isprovided to reinforce the strength of the vacuum adiabatic body, thesecond reinforcement member 110 is not provided separately. In thiscase, an inner protrusion 281 may be provided on the inner surface ofthe first plate member 10 so that the sealing frame 200 is coupled. Theinner protrusion 281 may be coupled to the first plate member 10 bywelding or fitting. This embodiment may be applied to a case in whichthe sufficient strength of the main body-side vacuum adiabatic body isobtained only by the reinforcement member provided in the firstreinforcement member 100, that is, the inside of the vacuum space part50, and the reinforcement member is installed on a side of the secondplate member 20.

The first member coupling groove 282 may be provided in the first membercoupling part 232 so as to be inserted and fixed to the inner protrusion281. The inner protrusion 281 may be inserted into the first membercoupling groove 282 so that a coupled position of the sealing frame 200is fixed.

Referring to FIG. 23 , it is characteristically different that the firstmember coupling groove 282 is not provided as compared with theembodiment shown in FIG. 22 . According to this embodiment, one end ofthe first member coupling part 232 may be supported by the innerprotrusion 281 so that the position of the sealing frame 200 issupported.

When compared to the embodiment proposed in FIG. 22 , this embodimentmay have a disadvantage in that the movement of the sealing frame 200 isstopped in only one direction, instead that the movement of the sealingframe 200 in the y-axis direction is stopped by the inner protrusion 281and the first member coupling groove 282 in both directions. However, anadvantage that the worker conveniently works when the sealing frame 200is coupled may be expected.

In the embodiment proposed in FISG. 19 to 23, a side of the first platemember 10 is fixed, and a side of the second plate member 20 is providedwith a constituent in which the movement such as sliding or the like isallowed. That is to say, the second plate member 20 and the outersurface part 210 are allowed to be relatively slidable, and relativemovement of the first plate member 10 and the inner surface part 230 isnot allowed. Such the constituent may be configured opposite to eachother. Hereinafter, such the constituent will be proposed.

Referring to FIG. 24 , an outer protrusion 283 may be provided on theouter surface of the second plate member 20, and an outer hook part 213may be provided on the outer surface 210 of the sealing frame 200. Theouter hook part 213 may be hooked to be supported by the outerprotrusion 283.

In case of this embodiment, the inner surface part 230 of the sealingframe 200 may be allowed to move with respect to the inner surface partof the first plate member 10 such as the sliding or the like. In thisembodiment, mounting and fixing of the sealing frame 200 are differentonly in the direction, and the same description may be applied.

Various embodiments may be further proposed in addition to theembodiment related to FIG. 24 . For example, the reinforcement member100 and 110 may be further provided on the second plate member 20, andvarious structures of FIGS. 19 to 21 may be provided for thereinforcement member. Also, the outer hook part 213 may be provided as agroove structure as shown in FIG. 22 .

According to this embodiment, there is a difference in configurationsuch that the coupling direction of the sealing frame 200 is provided inthe opposite direction of the original embodiment. However, thefundamental function of the sealing frame may be obtained in the sameway.

Hereinafter, an embodiment in which the adiabatic loss through the edgeportion of the vacuum adiabatic body, that is, the adiabatic loss due tothe leakage of cold air through the narrow gap of the plate member atthe edge of the vacuum adiabatic body is improved is disclosed. Also, arefrigerator to which the vacuum adiabatic body is applied will bedescribed. The description of the embodiments below may be applied tothe ideas disclosed in the previous embodiments. Therefore, even ifthere is no specific mention, the technical ideas of the other previousembodiments may be applied to the following embodiments within theallowable range.

FIG. 25 is an enlarged cross-sectional view illustrating a contact partbetween a door and a main body of the refrigerator as an edge portion ofa vacuum adiabatic body according to an embodiment.

Referring to FIG. 25 , a first plate member 10, a second plate member20, and a conductive resistance sheet 60 are provided. The conductiveresistance sheet 60 may be provided as a thin plate to resist to thermalconduction between the plate members 10 and 20. Although the conductiveresistance sheet 60 is provided as a flat plan shape as a thin plate,the conductive resistance sheet 60 may have a curved shape by beingpulled inward when vacuum is applied to the vacuum space part 50.

The conductive resistance sheet 60 is provided at an angle differentfrom that of the previous embodiment. In detail, when the plate members10 and 20 are viewed horizontally, the plate members 10 and 20 areinclined at an angle other than a predetermined angle. That is to say, avirtual line connecting both ends of the conductive resistance sheet toeach other with respect to the cross-section may be set at an arbitraryangle, not perpendicular to the extension direction of the plate member.In other words, a virtual line having the shortest distance, whichconnects end portions of the first plate member to the second platemember is set so that at least one extension direction of the firstplate member or the second plate member is obliquely inclined whenviewed in a horizontal direction. Thus, the length of the virtual lineconnecting the end portions of the plate members 10 and 20 is longerthan the width of the vacuum space part. In addition, the length of theside surface part of the sealing frame 200 and the length of the gasket80, which will be described below, are longer than the width of thevacuum space part.

According to an embodiment, it may be provided inwardly, that is,inclined to the inside of the refrigerator, at an acute angle inwardfrom the outside of the vacuum adiabatic body. That is, the end portionof the first plate member disposed inside the refrigerator is positionedinside the end portion of the second plate member outside therefrigerator.

According to the configuration of the conductive resistance sheet 60described above, the length of the conductive resistance sheet 60connecting the plate members 10 and 20 to each other becomes long, andan amount of conductive heat transmitted through the conductiveresistance sheet 60 is further reduced .

Since the conductive resistance sheet 60 has the thin plate shape andlow strength, the conductive resistance sheet 60 may be damaged by evenan external small impact. As a result, when the conductive resistancesheet 60 is damaged, the vacuum of the vacuum space part may be broken,and thus, performance of the vacuum adiabatic body may not be properlyexerted. To solve this limitation, a sealing frame 200 may be disposedto be inclined to the inside of the refrigerator on an outer surface ofthe conductive resistance sheet 60. According to the sealing frame 200,components of the door 3 or other components may not directly contactthe conductive resistance sheet 60 but indirectly contact the conductiveresistance sheet 60 through the sealing frame 200 to prevent theconductive resistance sheet 60 from being damaged. To allow the sealingframe 200 to prevent an impact from being applied to the conductiveresistance sheet 60, the two members may be spaced apart from eachother, and a buffer member may be interposed between the two members.

To reinforce the strength of the vacuum adiabatic body, a reinforcementmember may be provided on each of the plate members 10 and 20. Forexample, the reinforcement member may include a reinforcement member 110coupled to an edge portion of the first plate member 10. To improve thestrength of the vacuum adiabatic body, a member having a thickness andstrength greater than those of the plate member 10 may be applied to thereinforcement member 100. The reinforcement member may be installed withrespect to the second plate member as described in the foregoingembodiment.

The sealing frame 200 may include an inner surface part 230 disposed inthe internal space of the main body 2 and supported by the first platemember 10, an outer surface part 210 disposed in the external space ofthe main body 2 and supported by the second plate member 20, and a sidesurface part 220 disposed on a side surface of the edge of the vacuumadiabatic body constituting the main body 2 to cover the conductiveresistance sheet 60 and connect the inner surface part 230 to the outersurface part 210.

The side surface part 220 may be inclined inward in the extensiondirection of the conductive resistance sheet 60. An installation anglemay also be inclined like the conductive resistance sheet 60. Thus, aprotection action with respect to the conductive resistance sheet 60 maybe sufficiently achieved.

The sealing frame 200 provides a first plate member 10 for providing avacuum space and a cover member for an adiabatic space covering an endportion of the second plate member 20. At least a portion of the sidesurface part 220 of the sealing frame 200 has a first extension part onwhich the gasket 80 is seated when the door is closed.

The energy nose 500 may be provided in a gap part between the sidesurface part 220 of the sealing frame 200 and the door 3 and morespecifically the door liner 400. A portion of the sealing frame 200providing the energy nose may be called a second extension part. Thefirst extension part and the second extension part may be continuouslyconnected to each other. Thus, an adiabatic effect of the energy nosemay be improved.

The sealing frame 200 may be made of a resin material that is slightlydeformable. A mounted position of the sealing frame 200 may bemaintained by an interaction between the inner surface part 230 and theouter surface part 210, i.e., by a holding action. That is to say, theset position may not be separated.

A door liner 400 may be provided on the door 3. The door liner 400 iselongated toward the inside of the refrigerator when viewed incross-section. The extension length of the door liner 400 may beextended to the length of the side surface part 220 of the sealing frame200. That is to say, a door liner protrusion 420 may be disposed toextend to the side surface part 220 of the sealing frame 200. A gap partbetween the side surface portion 220 and the door liner protrusion 420forms an energy nose to further reduce heat loss.

A gasket 80 may be installed on the door liner 400. The gasket 80 may beprovided so that the length of the conductive resistance sheet 60becomes longer and longer. The gasket 80 can be fastened by inserting agasket fastening member or tool 83 into a door liner fastening groove410 provided in the door liner 400. The gasket 80 is provided with amagnet 82 so that the gap between the door 3 and the main body 2 issealed by force that the magnet 82 approaches the door.

The gasket 80 is disposed between the main body of the refrigerator andthe door to prevent the cold air from leaking between the door and themain body when the door is closed. The gasket 80 is inclined inward toallow the door to be compressed and deformed to be sealed between thedoor and the main body when the door is closed.

The gasket may have a body part including a gasket coupling tool 83 anda wing part provided in a thin plate shape and allowed to be deformed sothat the gasket is compressed and deformed. The gasket 80 may be made ofa highly elastic material so that the body and the wing are formed, andthe wing is deformed. A resin such as PVC may be used as the material ofthe gasket 80.

Table 1 shows the thermal conductivity of each component and materialapplied to the refrigerator.

TABLE 1 Material Thermal Conductivity (W/mK) Polyurethane foam 0.026 VIP0.0032 Al 202 Gasket 5 Steel 14.9 ABS 0.19 Rubber magnet 10 Air 0.024Vacuum adiabatic body 0.002

Referring to Table 1, polyurethane foam according to the related art hasthermal conductivity as high as 13 times as compared with a vacuumadiabatic body, of which the inside is maintained in a vacuum state,according to an embodiment. A vacuum insulation plate (VIP) in which aporous material is accommodated therein has thermal conductivity as highas about 25% as compared with the vacuum adiabatic body. The PVC hasthermal conductivity of about 0.16, similar to ABS. As a result, thethermal conductivity gradually increases in order of the vacuumadiabatic body, the polyurethane foam, and the PVC. A thickness of eachmember corresponding to the thermal conductivity of each member will bedescribed. First, the thickness of the vacuum adiabatic body may beabout 10 mm to about 20 mm to secure a wide internal space of therefrigerator. When the polyurethane foam is applied to secure the samedegree of adiabatic performance, a thickness of about 40 mm to about 50mm or more may be applied. In case of the gasket 80, it is difficult tosecure sufficient adiabatic performance with a thickness similar to thatof the vacuum adiabatic body. For this reason, the gasket 80 may beapplied with a width of about 20 mm to about 30 mm or more.

Sufficient adiabatic performance may be secured only when a width of asurface of the gasket 80, which contact the sealing frame 200 is greaterthan the width of the vacuum adiabatic body.

To secure the sufficient adiabatic performance, a maximum value of alength of the gasket in the horizontal direction that is parallel to thesurface on which the gasket 80 is seated on the sealing frame 200 may begreater than a gap between the first plate member 10 and the secondplate member 20, which define the third space.

A maximum value of a length of the sealing frame in the horizontaldirection that is parallel to the surface on which the gasket 80 isseated on the sealing frame may be greater than a gap between the firstplate member 10 and the second plate member 20, which define the thirdspace.

Specific operations of this embodiment will be described with referenceto the respective drawings.

First, FIG. 26 is a conceptual view of an energy nose in therefrigerator, and FIG. 27 is a view for comparing the energy noses of ageneral conductive resistance sheet and an inclined conductiveresistance sheet.

In FIG. 26 , a red color indicates a relatively high temperature, and ablue color indicates a relatively low temperature. Firstly, the leakageof cold air is blocked by the gasket in a space between the door and themain body. Furthermore, it is seen that the temperature suddenly changeseven in a narrow gap part toward the inside of the gasket. This narrowregion may be called an energy nose 501. The energy nose is a zone inwhich convection heat transfer is blocked because the forced air flow inthe refrigerator is blocked by the narrow gap.

In foregoing another embodiment shown in FIG. 27(a), it is seen that thespace of the gasket 80, which faces the inside of the refrigerator, isdifficult to provide the energy nose. On the other hand, in thisembodiment shown in FIG. 27(b), it is seen that the energy nose 500 isprovided in the space of the gasket 80, which faces the inside of therefrigerator. Thus, it is also possible to provide the energy nose evenin the refrigerator to which the vacuum adiabatic body is applied,thereby ensuring high adiabatic performance for the refrigerator.

Referring again to FIG. 25 , the conductive resistance sheet 60 isprovided to be inclined. The conductive resistance sheet is coupled tothe plate member through welding.

When the conductive resistance sheet is inclined at an angle withrespect to the plate member, it is difficult to secure adhesion betweenthe conductive resistance sheet and the plate member during the welding.The present inventor has taken note of the fact that the conductiveresistance sheet 60 is performed before the welding to solve thislimitation. The welding of the conductive resistance sheet and the platemember will be described in detail with reference to the drawings.

FIG. 28 is a view for explaining a welding device that welds aconductive resistance sheet to a plate member according to a relatedart.

Referring to FIG. 28 , in a welding apparatus 600, a plurality of jigsare placed inside the casing 510 which is divided into upper and lowerparts and left and right parts. A pair of lower jig 520 and upper jig530 are placed in the jig, and a conductive resistance sheet 60 isplaced in a gap between the upper jig 530 and the lower jig 520.

The upper side jig 530 includes an outer upper jig 531, a center upperjig 532, and an inner upper side jig 533. The gap part between the outerupper jig 531 and the center upper jig 532 and the gap part between thecenter upper jig 532 and the inner upper jig 533 are opened so thatlaser is introduced.

When explaining a welding process, first, in the welding apparatus, afirst plate member 10 and a second plate member 20 are disposed close toinner surfaces of the pair of lower jigs 520. A conductive resistancesheet 60 is disposed between the plate member and the upper jig. Thelaser is irradiated to the gap part between the upper jig to weld andfix the conductive resistance sheet 60 and the plate members 10 and 20to each other. Here, a negative pressure environment is formed in theinner space of the lower jig 520 so that the conductive resistance sheet60 and the plate members 10 and 20 are more closely attached to eachother.

As described above, the horizontal conductive resistance sheet accordingto the related art may be welded to the plate member by the weldingapparatus. To weld the inclined conductive resistance sheet according tothis embodiment, the center upper jig 532 is divided into left and rightparts, and the outer upper jig 531 moves upward relative to the innerupper jig 533 to perform the welding. Alternatively, the lower jig 520and the case 510 may have different positions and designs.

FIG. 29 is a view for comparing coupling processes of the conductiveresistance sheet according to the foregoing embodiment and theconductive resistance sheet according to this embodiment.

The conductive resistance sheet 60 of FIG. 29(a) according to therelated art is disposed in a horizontal state so that the weldingapparatus shown in FIG. 28 is applied as it is to perform the welding.

The bending-type conductive resistance sheet 65 according to thisembodiment shown in FIG. 29(b) is provided with a first bending part 652and a second bending part 653, which are respectively provided at bothend portions of the inclined part 651 provided at the center thereof.The first welding part 652 is aligned with a first support 11 providedat the end portion of the first plate member 10, and the second weldingpart 653 is provided at the end portion of the second plate member 20.

The plate member and the bending-type conductive resistance sheet may bewelded to each other by being inserted into the welding apparatus in thealignment state as described above.

According to this method, it is possible to secure the sealability ofthe coupling between the conductive resistance sheet and the platemember, and it is possible to expect an advantage of solving thelimitation of leakage due to the coupling between the conductive memberand the plate member.

Referring again to FIG. 25 , the gasket 80 is provided with a gasketcoupling member 83, and the gasket coupling member 83 is inserted intothe door liner coupling groove 410 to couple the gasket. The extensiondirection of the main body of the gasket 80 and the extension directionof the gasket coupling tool 83 are inclined at an angle α. This is forfacilitating the manufacture of the door liner.

This will be described with reference to the comparison drawing of FIG.3 .

FIG. 30(a) illustrates a state in which the gasket body and the gasketcoupling tool are perpendicular to each other as a comparative example,and FIG. 30(b) illustrates a state in which the gasket body and thegasket coupling tool are inclined at an angle α according to anembodiment. The comparative example of FIG. 30(a) is widely used as ageneral gasket construction.

Referring to FIG. 30(a), to insert the vertical gasket coupling tool 83,the door liner is provided with a recessed door liner coupling groove411 which is provided deep and large. The recessed door liner couplinggroove 411 is provided at a predetermined depth and width and in apredetermined direction for securing the coupling force of the gasket80.

When the recessed door liner coupling groove 411 is provided deeply andinclinedly as illustrated in the drawing, molding of the door liner isvery difficult.

In detail, the door liner 400 is provided through injection or vacuummolding. Here, the mold is used in which the mold is separated in onedirection, and the mold may be taken out in the one direction or in onedirection perpendicular to the one direction. However, the taking out ofthe mold may be impossible or very difficult in the direction ofinclination, which is not parallel or perpendicular to the onedirection.

It is impossible to take out the mold in a direction that is inclinedobliquely with respect to the door liner 400 as illustrated by the arrowin FIG. 30(a). The mold may easily be taken out in a directionperpendicular to the door liner 400 as shown by the arrow in FIG. 30(b).

To reflect the difficulty of such a manufacturing process, the gasketcoupling tool 83 is provided at an oblique angle, not be perpendicularto the extension direction of the may body of the gasket 80, butinclined at an angle α, and also, the door liner coupling grove 410 isprovided to be inclined at an angle α. Here, the angle α is inclined atan angle other than 90 degrees. The gasket coupling tool 83 and the doorliner coupling hole 410 are provided so that the conductive resistancesheet 60 is inclined at an angle.

According to the foregoing embodiment, the length of the conductiveresistance sheet may be longer than that of the interval between theplate members 10 and 20. The length of the conductive resistance sheetmay vary depending on the angle at which the conductive resistance sheetis inclined. Thus, the adiabatic performance may be improved by loweringthe conduction heat conducted along the conductive resistance sheet.Also, since the gasket is installed at a longer and wide interval, theadiabatic performance may be further improved, and energy nose may beprovided to obtain further improved adiabatic performance.

Particularly, since the energy nose is provided, it is possible togreatly improve the substantial adiabatic performance using a narrowspace, and it is possible to improve the adiabatic performance that isnot obtained in the case of the refrigerator using the vacuum adiabaticbody according to the related art.

The vacuum adiabatic body using the inclined conductive resistance sheetaccording to another embodiment is proposed. In the following otherembodiments, the inclination of the conductive resistance sheet isdifferent in the angular direction, and the other portions are the sameas the embodiment shown in FIG. 25 and the like. Thus, the descriptionthat may be applied will be applied equally to the followingembodiments.

FIG. 31 is an enlarged cross-sectional view illustrating a contact partbetween a door and a main body of the refrigerator as an edge portion ofa vacuum adiabatic body according to another embodiment.

Referring to FIG. 31 , a first plate member 10, a second plate member20, and a conductive resistance sheet 60 are provided. The conductiveresistance sheet 60 may be provided as a thin plate to resist to thermalconduction between the plate members 10 and 20. Although the conductiveresistance sheet 60 is provided as a flat plan shape as a thin plate,the conductive resistance sheet 60 may have a curved shape by beingpulled inward when vacuum is applied to the vacuum space part 50.

The conductive resistance sheet 60 is provided to be inclined. Indetail, the conductive resistance sheet 60 is provided to be inclinedobliquely at a predetermined angle but to be perpendicular to theextension direction of the plate members 10 and 20. Unlike theembodiment shown in FIG. 25 , it may be provided to be inclined outwardfrom the inside of the vacuum adiabatic body to an acute angleoutwardly.

The sealing frame 200, the gasket 80, the energy nose 500, and the likeare provided as in the embodiment of FIG. 25 . However, an edge portionof the door 3 is wider outward than an edge portion of the main body 2by w. Due to this difference in structure, there is a difference in thestructure and action as follows.

Particularly, the gasket 80 is provided to be inclined to the outside ofthe refrigerator like the vacuum adiabatic body. The sealing frame 200is provided to the outside of the refrigerator, i.e., to be inclinedoutward from the inside of the vacuum adiabatic body. The sealing frame200 provides a first plate member 10 for providing a vacuum space and acover member for an adiabatic space covering an end portion of thesecond plate member 20. At least a portion of the side surface part 220of the sealing frame 200 has a first extension part on which the gasket80 is seated when the door is closed.

The energy nose 500 may be provided in a gap part between the firstplate member 10 and the door 3, more particularly, the door liner 400.

According to this embodiment, it is not necessary to provide the longsealing frame so as to obtain the energy nose, and the first platemember may be used as one surface of the energy nose. Also, therefrigerator according to this embodiment may be applied to therefrigerator in which the main body is inserted into the refrigeratorinstallation space, and only the door protrudes.

INDUSTRIAL APPLICABILITY

The vacuum adiabatic body and the refrigerator according to theembodiments may solve the above limitations according to the relatedart, which does not provide the energy nose, and the conductiveresistance sheet may increase in length to reduce the conductive heattransfer amount and improve the adiabatic effect due to the contactbetween the members, thereby further approaching the practicalindustrial application of the device using the vacuum adiabatic body.

What is claimed is:
 1. A refrigerator comprising: a main body having avacuum adiabatic body to form a storage space, wherein the vacuumadiabatic body includes: a first plate; and a second plate, at least aportion of the second plate being spaced apart from the first plate in afirst direction to define a vacuum space between the first plate and thesecond plate; a door provided to open and close an opening of the mainbody to allow access to the storage space; a gasket installed on one ofthe door or the main body; and a frame provided between the vacuum spaceand a portion of the door, the frame including a wall that contacts thegasket when the door closes the opening and that separates from thegasket when the door opens the opening, wherein the wall of the framehas a surface that is inclined with respect to an extension direction ofat least one of the first plate or the second plate.
 2. The refrigeratoraccording to claim 1, further comprising a heat resistance sheet that iscoupled to at least one of the first plate or the second plate, whereinthe frame is provided to cover the heat resistance sheet.
 3. Therefrigerator according to claim 1, wherein the wall of the frameincludes: a first region on which the gasket is seated when the door isclosed; and a second region configured to provide an air gap between theframe and the door when the door is closed.
 4. The refrigeratoraccording to claim 3, wherein at least a portion of the second region isinclined with respect to the extension direction of at least one of thefirst plate or the second plate.
 5. The refrigerator according to claim1, wherein a distance between the first plate and the second plate inthe first direction is less than a width of the gasket in the firstdirection.
 6. The refrigerator according to claim 1, wherein a distancebetween the first plate and the second plate in the first direction isless than a width of the frame in the first direction.
 7. Therefrigerator according to claim 2, wherein the heat resistance sheet hasa surface inclined with respect to the extension direction of at leastone of the first plate or the second plate.
 8. The refrigeratoraccording to claim 7, wherein the heat resistance sheet includes: afirst welding surface extending from a first end of the surface of theheat resistance sheet, the first welding surface being welded to thefirst plate; and a second welding surface extending from a second end ofthe surface of the heat resistance sheet, the second welding surfacebeing welded to the second plate.
 9. The refrigerator according to claim8, wherein each of the first plate and the second plate includes an endadjacent to the frame, and wherein one of the end of the first plate orthe end of the second plate further protrudes with respect to anotherone of the end of the first plate or the end of the second plate. 10.The refrigerator according to claim 1, wherein the frame includes: aninner surface wall positioned to correspond to a portion of the firstplate; and an outer surface wall positioned to correspond to a portionthe second plate; wherein the wall that is inclined is provided betweenthe inner surface wall and the outer surface wall.
 11. The refrigeratoraccording to claim 10, wherein at least a portion of the inner surfacewall extends in a different direction than the outer surface wall. 12.The refrigerator according to claim 10, wherein at a portion of theinner surface wall extends in a different direction from the extensiondirection of the first plate.
 13. The refrigerator according to claim10, wherein at least a portion of the outer surface wall has anextension direction that corresponds to the extension direction of thesecond plate.
 14. A refrigerator comprising: a main body having a vacuumadiabatic body to form a storage space, wherein the vacuum adiabaticbody includes: a first plate; and a second plate, at least a portion ofthe second plate being spaced apart from the first plate in a firstdirection to define a vacuum space between the first plate and thesecond plate; a door provided to open and close an opening of the mainbody to allow access to the storage space; a gasket installed on one ofthe door or the main body; and a frame provided between the vacuum spaceand a portion of the door, the frame including a wall that contacts thegasket when the door closes the opening and that separates from thegasket when the door opens the opening, wherein the gasket includes: agasket body contacting the frame to seal between the door and the mainbody when the door is closed, at least a portion of the gasket bodybeing inclined with respect to an extension direction of at least one ofthe first plate or the second plate.
 15. The refrigerator according toclaim 14, wherein the gasket includes a gasket coupling end that isprovided to be obliquely inclined with respect to an extension directionof the gasket body.
 16. The vacuum adiabatic body according to claim 14,wherein each of the first plate and the second plate includes an endadjacent to the frame, and wherein the wall extends substantiallyparallel to a line between the end of the first plate and the end of thesecond plate.
 17. A vacuum adiabatic body comprising: a main body havinga vacuum adiabatic body to form a storage space configured to storeitems, wherein the vacuum adiabatic body includes: a first plate; and asecond plate, at least a portion of the second plate being spaced apartfrom the first plate in a first direction to define a vacuum spacebetween the first plate and the second plate; a gasket installed on oneof the door or the main body; and a frame provided between the vacuumspace and a portion of the door, the frame including a wall thatcontacts the gasket when the door closes the opening, wherein the wallis spaced apart from and does not contact the first and second plates.18. The refrigerator according to claim 17, wherein the wall of theframe is obliquely inclined toward the storage space inside the mainbody with respect to an extension direction of at least one of the firstplate or the second plate.
 19. The refrigerator according to claim 17,wherein the gasket includes: a gasket body contacting the frame to sealbetween the door and the main body when the door is closed; and a gasketcoupling end provided to be obliquely inclined with respect to anextension direction of the gasket body.
 20. The refrigerator accordingto claim 17, wherein the wall includes a first region on which thegasket is seated when the door is closed and a second region configuredto provide an air gap between the door and the frame when the door isclosed.